ANALYSIS AND TESTS OF REINFORCED CARBON-EPOXY FOAM-CORE SANDWICH PANELS WITH CUTOUTS/

Authors
Citation
Dj. Baker et C. Rogers, ANALYSIS AND TESTS OF REINFORCED CARBON-EPOXY FOAM-CORE SANDWICH PANELS WITH CUTOUTS/, Journal of the American Helicopter Society, 43(2), 1998, pp. 120-132
Citations number
4
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
00028711
Volume
43
Issue
2
Year of publication
1998
Pages
120 - 132
Database
ISI
SICI code
0002-8711(1998)43:2<120:AATORC>2.0.ZU;2-V
Abstract
The results of a structurally-efficient minimum-gage shear-panel ape p resented. The shear-panel design is based on an Integrally stiffened s yntactic-foam stabilized-skin concept with an all-bias-ply tape constr uction for the skins. The panels considered in the study were designed to be buckling resistant up to 100 lbs/in. of shear load and to have an ultimate strength of 300 lbs/in. The experimental buckling strength of the reinforced panels is 83 to 90 percent of the predicted bucklin g strength based on a linear buckling analysis. The maximum experiment al deflection exceeds the maximum deflection predicted by a nonlinear analysis by approximately one panel thickness. The failure strength of the reinforced panels was two and a half to four times the buckling s trength. This efficient shear-panel design concept exceeds the require d ultimate strength requirement of 300 lbs/in. by over 100 percent.